REDEFINING THE LAUNCH INDUSTRY: HIGH-MAGNITUDE ELECTROMAGNETIC PROPULSION
- Paper number
IAC-08.D4.1.3
- Author
Mr. Justin Park, International Space University (ISU), United States
- Year
2008
- Abstract
This short thesis forecasts the utility of using electromagnetic propulsion as a means of launching lightweight payloads, such as small satellites, into lower earth orbit. The engineering constraints and possible methods of implementation are discussed briefly in this analysis, but the spotlight is placed primarily on the economic benefits of a high-magnitude electromagnetic propulsion system. No physical tests were conducted during this case study but the results of more than a dozen scientific experiments were used in the literature review. The hypothetical design described is unique because it contains new techniques to eliminate technical inefficiencies, reduce costs, and maximize carrying capacity. The conclusion is that financers will see a positive return on investment within four to six years. This type of high-altitude, superconducting cannon can be used multiple times a day to bring down the price to launch inflatable space station modules by several orders of magnitude, thus redefining the space industry at a very fundamental level.
- Abstract document
- Manuscript document
IAC-08.D4.1.3.pdf (🔒 authorized access only).
To get the manuscript, please contact IAF Secretariat.